Renewable Polyester Compositions having a Low Density

ABSTRACT

A thermoplastic composition that contains a rigid renewable polyester and has a voided structure and low density is provided. To achieve such a structure, the renewable polyester is blended with a polymeric toughening additive to form a precursor material in which the toughening additive can be dispersed as discrete physical domains within a continuous matrix of the renewable polyester. The precursor material is thereafter stretched or drawn at a temperature below the glass transition temperature of the polyester (i.e., “cold drawn”). This creates a network of voids located adjacent to the discrete domains, which as a result of their proximal location, can form a bridge between the boundaries of the voids and act as internal structural “hinges” that help stabilize the network and increase its ability to dissipate energy. The present inventors have also discovered that the voids can be distributed in a substantially homogeneous fashion throughout the composition.

BACKGROUND OF THE INVENTION

Molding processes are commonly used to form plastic articles that are relatively rigid in nature, including containers, medical devices, and so forth. For example, containers for stacks or rolls of pre-moistened wipes are generally formed by injection molding. One problem associated with such containers, however, is that the molding material is often formed from synthetic polyolefins (e.g., polypropylene or HDPE) that are not renewable. Various attempts have thus been made to use renewable polyesters (e.g., polylactic acid (“PLA”)) in these and other applications. However, market penetration of renewable polyesters has been limited due to a density that is approximately 30% higher than conventional polyolefins, which makes them significantly more expensive. To help reduce the density of such polyesters, gaseous blowing agents are sometimes employed to help create a cellular “foamed” structure having a certain degree of porosity. Unfortunately, however, the processability and tensile properties of the resulting cellular structure is often compromised due to the uncontrolled pore size and distribution. Other problems also exist. Renewable polyesters, for example, have a relatively high glass transition temperature and typically demonstrate a very high stiffness and tensile modulus, while having relatively low impact resistance and low ductility/elongations at break. As an example, polylactic acid has a glass transition temperature of about 59° C. and a tensile modulus of about 2 GPa or more. Nevertheless, the tensile elongation (at break) for PLA materials are only about 5%, and the notched impact strength is only about 0.22 J/cm. Such low impact strength and tensile elongation values significantly limit the use of such polymers in injection molded parts, where a good balance between material stiffness and impact strength is required.

As such, a need currently exists for a low density renewable polyester composition that can also demonstrate a high resistance to failure when subjected to stress.

SUMMARY OF THE INVENTION

In accordance with one embodiment of the present invention, a thermoplastic composition is disclosed that comprises at least one rigid renewable polyester having a glass transition temperature of about 0° C. or more and at least one polymeric toughening additive. The thermoplastic composition has a morphology in which a plurality of discrete primary domains and voids are dispersed within a continuous phase, the domains containing the polymeric toughening additive and the continuous phase containing the renewable polyester. The thermoplastic composition has a density of about 1.4 grams per cubic centimeter or less. The average percent volume of the composition that is occupied by the voids is from about 20% to about 80% per cubic centimeter.

In accordance with another embodiment of the present invention, a method for forming a low density thermoplastic composition for use in a molded article is disclosed. The method comprises forming a blend that contains a rigid renewable polyester and a polymeric toughening additive, wherein the rigid renewable polyester has a glass transition temperature of about 0° C. or more. The blend is formed into the shape of a precursor material. The precursor material is stretched at a temperature that is lower than the glass transition temperature of the renewable polyester to form a thermoplastic composition that contains a plurality of voids and has a density of about 1.4 grams per cubic centimeter or less.

Other features and aspects of the present invention are discussed in greater detail below.

BRIEF DESCRIPTION OF THE DRAWINGS

A full and enabling disclosure of the present invention, including the best mode thereof, directed to one of ordinary skill in the art, is set forth more particularly in the remainder of the specification, which makes reference to the appended figures in which:

FIG. 1 is a schematic illustration of one embodiment of an injection molding apparatus for use in the present invention;

FIG. 2 is an SEM photomicrograph of a sample of Example 7 after cold drawing and oxygen plasma etching;

FIG. 3 is an SEM photomicrograph of a sample of Example 8 after cold drawing and impact testing;

FIG. 4 is an SEM photomicrograph of a sample of Example 11 before cold drawing; and

FIG. 5 is an SEM photomicrograph of a sample of Example 11 after cold drawing; and

FIG. 6 is an SEM photomicrograph of a sample of Example 11 after cold drawing and oxygen plasma etching.

Repeat use of references characters in the present specification and drawings is intended to represent same or analogous features or elements of the invention.

DETAILED DESCRIPTION OF REPRESENTATIVE EMBODIMENTS

Reference now will be made in detail to various embodiments of the invention, one or more examples of which are set forth below. Each example is provided by way of explanation of the invention, not limitation of the invention. In fact, it will be apparent to those skilled in the art that various modifications and variations may be made in the present invention without departing from the scope or spirit of the invention. For instance, features illustrated or described as part of one embodiment, may be used on another embodiment to yield a still further embodiment. Thus, it is intended that the present invention covers such modifications and variations as come within the scope of the appended claims and their equivalents.

Generally speaking, the present invention is directed to a thermoplastic composition that contains a rigid renewable polyester and has a voided structure and low density. To achieve such a structure, the renewable polyester is blended with a polymeric toughening additive to form a precursor material in which the toughening additive can be dispersed as discrete physical domains within a continuous matrix of the renewable polyester. The precursor material is thereafter stretched or drawn at a temperature below the glass transition temperature of the polyester (i.e., “cold drawn”). Without intending to be limited by theory, the present inventors believe that the deformation force and elongational strain of the drawing process causes debonding to occur in the renewable polyester matrix at those areas located adjacent to the discrete domains. This creates a network of voids (e.g., voids, nano-voids, or a combination thereof) located adjacent to the discrete domains, which as a result of their proximal location, can form a bridge between the boundaries of the voids and act as internal structural “hinges” that help stabilize the network and increase its ability to dissipate energy.

The average percent volume occupied by the voids within a given unit volume of the thermoplastic composition is relatively high, such as from about 20% to about 80% per cm³, in some embodiments from about 30% to about 70%, and in some embodiments, from about 40% to about 60% per cubic centimeter of the composition. Such a high void volume can significantly lower the density of the material. For example, the composition may have a density of about 1.4 grams per cubic centimeter (“g/cm³”) or less, in some embodiments about 1.1 g/cm³ or less, in some embodiments from about 0.4 g/cm³ to about 1.0 g/cm³, and in some embodiments, from about 0.5 g/cm³ to about 0.95 g/cm³. The present inventors have also discovered that the voids can be distributed in a substantially homogeneous fashion throughout the composition. For example, the voids may be distributed in columns that are oriented in a direction generally perpendicular to the direction in which a stress is applied. These columns may be generally parallel to each other across the width of the composition. Without intending to be limited by theory, it is believed that the presence of such a homogeneously distributed voided network can result in in significant energy dissipation under load and a significantly enhanced impact strength. This is in stark contrast to conventional techniques for creating voids that involve the use of blowing agents to initiate pore formation, which tend to result in an uncontrolled pore distribution and poor mechanical properties.

Various embodiments of the present invention will now be described in more detail.

I. Thermoplastic Composition

A. Renewable Polyester

Renewable polyesters typically constitute from about 70 wt. % to about 99 wt. %, in some embodiments from about 75 wt. % to about 98 wt. %, and in some embodiments, from about 80 wt. % to about 95 wt. % of the thermoplastic composition. Any of a variety of renewable polyesters may generally be employed in the thermoplastic composition, such as aliphatic polyesters, such as polycaprolactone, polyesteramides, polylactic acid (PLA) and its copolymers, polyglycolic acid, polyalkylene carbonates (e.g., polyethylene carbonate), poly-3-hydroxybutyrate (PHB), poly-3-hydroxyvalerate (PHV), poly-3-hydroxybutyrate-co-4-hydroybutyrate, poly-3-hydroxybutyrate-co-3-hydroxyvalerate copolymers (PHBV), poly-3-hydroxybutyrate-co-3-hydroxyhexanoate, poly-3-hydroxybutyrate-co-3-hydroxyoctanoate, poly-3-hydroxybutyrate-co-3-hydroxydecanoate, poly-3-hydroxybutyrate-co-3-hydroxyoctadecanoate, and succinate-based aliphatic polymers (e.g., polybutylene succinate, polybutylene succinate adipate, polyethylene succinate, etc.); aliphatic-aromatic copolyesters (e.g., polybutylene adipate terephthalate, polyethylene adipate terephthalate, polyethylene adipate isophthalate, polybutylene adipate isophthalate, etc.); aromatic polyesters (e.g., polyethylene terephthalate, polybutylene terephthalate, etc.); and so forth.

Typically, the thermoplastic composition contains at least one renewable polyester that is rigid in nature and thus has a relatively high glass transition temperature. For example, the glass transition temperature (“T_(g)”) may be about 0° C. or more, in some embodiments from about 5° C. to about 100° C., in some embodiments from about 30° C. to about 80° C., and in some embodiments, from about 50° C. to about 75° C. The renewable polyester may also have a melting temperature of from about 140° C. to about 260° C., in some embodiments from about 150° C. to about 250° C., and in some embodiments, from about 160° C. to about 220° C. The melting temperature may be determined using differential scanning calorimetry (“DSC”) in accordance with ASTM D-3417. The glass transition temperature may be determined by dynamic mechanical analysis in accordance with ASTM E1640-09.

One particularly suitable rigid polyester is polylactic acid, which may generally be derived from monomer units of any isomer of lactic acid, such as levorotory-lactic acid (“L-lactic acid”), dextrorotatory-lactic acid (“D-lactic acid”), meso-lactic acid, or mixtures thereof. Monomer units may also be formed from anhydrides of any isomer of lactic acid, including L-lactide, D-lactide, meso-lactide, or mixtures thereof. Cyclic dimers of such lactic acids and/or lactides may also be employed. Any known polymerization method, such as polycondensation or ring-opening polymerization, may be used to polymerize lactic acid. A small amount of a chain-extending agent (e.g., a diisocyanate compound, an epoxy compound or an acid anhydride) may also be employed. The polylactic acid may be a homopolymer or a copolymer, such as one that contains monomer units derived from L-lactic acid and monomer units derived from D-lactic acid. Although not required, the rate of content of one of the monomer unit derived from L-lactic acid and the monomer unit derived from D-lactic acid is preferably about 85 mole % or more, in some embodiments about 90 mole % or more, and in some embodiments, about 95 mole % or more. Multiple polylactic acids, each having a different ratio between the monomer unit derived from L-lactic acid and the monomer unit derived from D-lactic acid, may be blended at an arbitrary percentage. Of course, polylactic acid may also be blended with other types of polymers (e.g., polyolefins, polyesters, etc.).

In one particular embodiment, the polylactic acid has the following general structure:

One specific example of a suitable polylactic acid polymer that may be used in the present invention is commercially available from Biomer, Inc. of Krailling, Germany) under the name BIOMER™ L9000. Other suitable polylactic acid polymers are commercially available from Natureworks LLC of Minnetonka, Minn. (NATUREWORKS®) or Mitsui Chemical (LACEA™). Still other suitable polylactic acids may be described in U.S. Pat. Nos. 4,797,468; 5,470,944; 5,770,682; 5,821,327; 5,880,254; and 6,326,458, which are incorporated herein in their entirety by reference thereto for all purposes.

The polylactic acid typically has a number average molecular weight (“M_(n)”) ranging from about 40,000 to about 160,000 grams per mole, in some embodiments from about 50,000 to about 140,000 grams per mole, and in some embodiments, from about 80,000 to about 120,000 grams per mole. Likewise, the polymer also typically has a weight average molecular weight (“M_(w)”) ranging from about 80,000 to about 200,000 grams per mole, in some embodiments from about 100,000 to about 180,000 grams per mole, and in some embodiments, from about 110,000 to about 160,000 grams per mole. The ratio of the weight average molecular weight to the number average molecular weight (“M_(w)/M_(n)”), i.e., the “polydispersity index”, is also relatively low. For example, the polydispersity index typically ranges from about 1.0 to about 3.0, in some embodiments from about 1.1 to about 2.0, and in some embodiments, from about 1.2 to about 1.8. The weight and number average molecular weights may be determined by methods known to those skilled in the art.

The polylactic acid may also have an apparent viscosity of from about 50 to about 600 Pascal seconds (Pa·s), in some embodiments from about 100 to about 500 Pa·s, and in some embodiments, from about 200 to about 400 Pa·s, as determined at a temperature of 190° C. and a shear rate of 1000 sec⁻¹. The melt flow rate of the polylactic acid (on a dry basis) may also range from about 0.1 to about 40 grams per 10 minutes, in some embodiments from about 0.5 to about 20 grams per 10 minutes, and in some embodiments, from about 5 to about 15 grams per 10 minutes, determined at a load of 2160 grams and at 190° C.

Some types of neat polyesters (e.g., polylactic acid) can absorb water from the ambient environment such that it has a moisture content of about 500 to 600 parts per million (“ppm”), or even greater, based on the dry weight of the starting polylactic acid. Moisture content may be determined in a variety of ways as is known in the art, such as in accordance with ASTM D 7191-05, such as described below. Because the presence of water during melt processing can hydrolytically degrade the polyester and reduce its molecular weight, it is sometimes desired to dry the polyester prior to blending. In most embodiments, for example, it is desired that the renewable polyester have a moisture content of about 300 parts per million (“ppm”) or less, in some embodiments about 200 ppm or less, in some embodiments from about 1 to about 100 ppm prior to blending with the toughening additive. Drying of the polyester may occur, for instance, at a temperature of from about 50° C. to about 100° C., and in some embodiments, from about 70° C. to about 80° C.

B. Polymeric Toughening Additive

As indicated above, the thermoplastic composition of the present invention also contains a polymeric toughening additive. Due to its polymeric nature, the toughening additive possesses a relatively high molecular weight that can help improve the melt strength and stability of the thermoplastic composition. Although not required, the polymeric toughening additive may be generally immiscible with the renewable polyester. In this manner, the toughening additive can better become dispersed as discrete phase domains within a continuous phase of the renewable polyester. The discrete domains are capable of absorbing energy that arises from an external force, which increases the overall toughness and strength of the resulting material. The domains may have a variety of different shapes, such as elliptical, spherical, cylindrical, etc. In one embodiment, for example, the domains have a substantially elliptical shape. The physical dimension of an individual domain is typically small enough to minimize the propagation of cracks through the polymer material upon the application of an external stress, but large enough to initiate microscopic plastic deformation and allow for shear zones at and around particle inclusions.

While the polymers may be immiscible, the toughening additive may nevertheless be selected to have a solubility parameter that is relatively similar to that of the renewable polyester. This can improve the interfacial compatibility and physical interaction of the boundaries of the discrete and continuous phases, and thus reduces the likelihood that the composition will fracture. In this regard, the ratio of the solubility parameter for the renewable polyester to that of the toughening additive is typically from about 0.5 to about 1.5, and in some embodiments, from about 0.8 to about 1.2. For example, the polymeric toughening additive may have a solubility parameter of from about 15 to about 30 MJoules¹²/m^(3/2), and in some embodiments, from about 18 to about 22 MJoules^(1/2)/m^(3/2), while polylactic acid may have a solubility parameter of about 20.5 MJoules^(1/2)/m^(3/2). The term “solubility parameter” as used herein refers to the “Hildebrand Solubility Parameter”, which is the square root of the cohesive energy density and calculated according to the following equation:

δ=√{square root over (()}(ΔH _(v) −RT)/V _(m))

where:

-   -   ΔHv=heat of vaporization     -   R=Ideal Gas constant     -   T=Temperature     -   Vm=Molecular Volume

The Hildebrand solubility parameters for many polymers are also available from the Solubility Handbook of Plastics, by Wyeych (2004), which is incorporated herein by reference.

The polymeric toughening additive may also have a certain melt flow rate (or viscosity) to ensure that the discrete domains and resulting voids can be adequately maintained. For example, if the melt flow rate of the toughening additive is too high, it tends to flow and disperse uncontrollably through the continuous phase. This results in lamellar or plate-like domains that are difficult to maintain and also likely to prematurely fracture. Conversely, if the melt flow rate of the toughening additive is too low, it tends to clump together and form very large elliptical domains, which are difficult to disperse during blending. This may cause uneven distribution of the toughening additive through the entirety of the continuous phase. In this regard, the present inventors have discovered that the ratio of the melt flow rate of the toughening additive to the melt flow rate of the renewable polyester is typically from about 0.2 to about 8, in some embodiments from about 0.5 to about 6, and in some embodiments, from about 1 to about 5. The polymeric toughening additive may, for example, have a melt flow rate of from about 0.1 to about 250 grams per 10 minutes, in some embodiments from about 0.5 to about 200 grams per 10 minutes, and in some embodiments, from about 5 to about 150 grams per 10 minutes, determined at a load of 2160 grams and at 190° C.

In addition to the properties noted above, the mechanical characteristics of the polymeric toughening additive may also be selected to achieve the desired increase in toughness. For example, when a blend of the renewable polyester and toughening additive is applied with an external force, shear and/or plastic yielding zones may be initiated at and around the discrete phase domains as a result of stress concentrations that arise from a difference in the elastic modulus of the toughening additive and renewable polyester. Larger stress concentrations promote more intensive localized plastic flow at the domains, which allows them to become significantly elongated when stresses are imparted. These elongated domains allow the composition to exhibit a more pliable and softer behavior than the otherwise rigid polyester resin. To enhance the stress concentrations, the toughening additive is selected to have a relatively low Young's modulus of elasticity in comparison to the renewable polyester. For example, the ratio of the modulus of elasticity of the renewable polyester to that of the toughening additive is typically from about 1 to about 250, in some embodiments from about 2 to about 100, and in some embodiments, from about 2 to about 50. The modulus of elasticity of the toughening additive may, for instance, range from about 2 to about 500 Megapascals (MPa), in some embodiments from about 5 to about 300 MPa, and in some embodiments, from about 10 to about 200 MPa. To the contrary, the modulus of elasticity of polylactic acid is typically from about 800 MPa to about 2000 MPa.

To impart the desired increase in toughness, the polymeric toughening additive may also exhibit an elongation at break (i.e., the percent elongation of the polymer at its yield point) greater than the renewable polyester. For example, the polymeric toughening additive of the present invention may exhibit an elongation at break of about 50% or more, in some embodiments about 100% or more, in some embodiments from about 100% to about 2000%, and in some embodiments, from about 250% to about 1500%.

While a wide variety of polymeric additives may be employed that have the properties identified above, particularly suitable examples of such polymers may include, for instance, polyolefins (e.g., polyethylene, polypropylene, polybutylene, etc.); styrenic copolymers (e.g., styrene-butadiene-styrene, styrene-isoprene-styrene, styrene-ethylene-propylene-styrene, styrene-ethylene-butadiene-styrene, etc.); polytetrafluoroethylenes; polyesters (e.g., recycled polyester, polyethylene terephthalate, etc.); polyvinyl acetates (e.g., poly(ethylene vinyl acetate), polyvinyl chloride acetate, etc.); polyvinyl alcohols (e.g., polyvinyl alcohol, poly(ethylene vinyl alcohol), etc.); polyvinyl butyrals; acrylic resins (e.g., polyacrylate, polymethylacrylate, polymethylmethacrylate, etc.); polyamides (e.g., nylon); polyvinyl chlorides; polyvinylidene chlorides; polystyrenes; polyurethanes; etc. Suitable polyolefins may, for instance, include ethylene polymers (e.g., low density polyethylene (“LDPE”), high density polyethylene (“HDPE”), linear low density polyethylene (“LLDPE”), etc.), propylene homopolymers (e.g., syndiotactic, atactic, isotactic, etc.), propylene copolymers, and so forth.

In one particular embodiment, the polymer is a propylene polymer, such as homopolypropylene or a copolymer of propylene. The propylene polymer may, for instance, be formed from a substantially isotactic polypropylene homopolymer or a copolymer containing equal to or less than about 10 wt. % of other monomer, i.e., at least about 90% by weight propylene. Such homopolymers may have a melting point of from about 160° C. to about 170° C.

In still another embodiment, the polyolefin may be a copolymer of ethylene or propylene with another α-olefin, such as a C₃-C₂₀ α-olefin or C₃-C₁₂ α-olefin. Specific examples of suitable α-olefins include 1-butene; 3-methyl-1-butene; 3,3-dimethyl-1-butene; 1-pentene; 1-pentene with one or more methyl, ethyl or propyl substituents; 1-hexene with one or more methyl, ethyl or propyl substituents; 1-heptene with one or more methyl, ethyl or propyl substituents; 1-octene with one or more methyl, ethyl or propyl substituents; 1-nonene with one or more methyl, ethyl or propyl substituents; ethyl, methyl or dimethyl-substituted 1-decene; 1-dodecene; and styrene. Particularly desired α-olefin comonomers are 1-butene, 1-hexene and 1-octene. The ethylene or propylene content of such copolymers may be from about 60 mole % to about 99 mole %, in some embodiments from about 80 mole % to about 98.5 mole %, and in some embodiments, from about 87 mole % to about 97.5 mole %. The α-olefin content may likewise range from about 1 mole % to about 40 mole %, in some embodiments from about 1.5 mole % to about 15 mole %, and in some embodiments, from about 2.5 mole % to about 13 mole %.

Exemplary olefin copolymers for use in the present invention include ethylene-based copolymers available under the designation EXACT™ from ExxonMobil Chemical Company of Houston, Tex. Other suitable ethylene copolymers are available under the designation ENGAGE™, AFFINITY™, DOWLEX™ (LLDPE) and ATTANE™ (ULDPE) from Dow Chemical Company of Midland, Mich. Other suitable ethylene polymers are described in U.S. Pat. No. 4,937,299 to Ewen et al.; U.S. Pat. No. 5,218,071 to Tsutsui et al.; U.S. Pat. No. 5,272,236 to Lai et al.; and U.S. Pat. No. 5,278,272 to Lai, et al., which are incorporated herein in their entirety by reference thereto for all purposes. Suitable propylene copolymers are also commercially available under the designations VISTAMAXX™ from ExxonMobil Chemical Co. of Houston, Tex.; FINA™ (e.g., 8573) from Atofina Chemicals of Feluy, Belgium; TAFMER™ available from Mitsui Petrochemical Industries; and VERSIFY™ available from Dow Chemical Co. of Midland, Mich. Other examples of suitable propylene polymers are described in U.S. Pat. No. 6,500,563 to Datta, et al.; U.S. Pat. No. 5,539,056 to Yang, et al.; and U.S. Pat. No. 5,596,052 to Resconi, et al., which are incorporated herein in their entirety by reference thereto for all purposes.

Any of a variety of known techniques may generally be employed to form the olefin copolymers. For instance, olefin polymers may be formed using a free radical or a coordination catalyst (e.g., Ziegler-Natta). Preferably, the olefin polymer is formed from a single-site coordination catalyst, such as a metallocene catalyst. Such a catalyst system produces ethylene copolymers in which the comonomer is randomly distributed within a molecular chain and uniformly distributed across the different molecular weight fractions. Metallocene-catalyzed polyolefins are described, for instance, in U.S. Pat. No. 5,571,619 to McAlpin et al.; U.S. Pat. No. 5,322,728 to Davis et al.; U.S. Pat. No. 5,472,775 to Obiieski et al.; U.S. Pat. No. 5,272,236 to Lai et al.; and U.S. Pat. No. 6,090,325 to Wheat, et al., which are incorporated herein in their entirety by reference thereto for all purposes. Examples of metallocene catalysts include bis(n-butylcyclopentadienyl)titanium dichloride, bis(n-butylcyclopentadienyl)zirconium dichloride, bis(cyclopentadienyl)scandium chloride, bis(indenyl)zirconium dichloride, bis(methylcyclopentadienyl)titanium dichloride, bis(methylcyclopentadienyl)zirconium dichloride, cobaltocene, cyclopentadienyltitanium trichloride, ferrocene, hafnocene dichloride, isopropyl(cyclopentadienyl,-1-flourenyl)zirconium dichloride, molybdocene dichloride, nickelocene, niobocene dichloride, ruthenocene, titanocene dichloride, zirconocene chloride hydride, zirconocene dichloride, and so forth. Polymers made using metallocene catalysts typically have a narrow molecular weight range. For instance, metallocene-catalyzed polymers may have polydispersity numbers (M_(w)/M_(n)) of below 4, controlled short chain branching distribution, and controlled isotacticity.

Regardless of the materials employed, the relative percentage of the polymeric toughening additive in the thermoplastic composition is selected to achieve the desired properties without significantly impacting the renewability of the resulting composition. For example, the toughening additive is typically employed in an amount of from about 1 wt. % to about 30 wt. %, in some embodiments from about 2 wt. % to about 25 wt. %, and in some embodiments, from about 5 wt. % to about 20 wt. % of the thermoplastic composition, based on the weight of the renewable polyesters employed in the composition. The concentration of the toughening additive in the entire thermoplastic composition may likewise constitute from about 0.1 wt. % to about 30 wt. %, in some embodiments from about 0.5 wt. % to about 25 wt. %, and in some embodiments, from about 1 wt. % to about 20 wt. %.

C. Interphase Modifier

An interphase modifier may also be employed in the thermoplastic composition to reduce the degree of friction and connectivity between the toughening additive and renewable polyester, and thus enhance the degree and uniformity of debonding. In this manner, the voids can be distributed in a substantially homogeneous fashion throughout the composition. The modifier is generally in a liquid or semi-solid form at room temperature (e.g., 25° C.) so that it possesses a relatively low viscosity, allowing it to be more readily incorporated into the thermoplastic composition and to easily migrate to the polymer surfaces. In this regard, the kinematic viscosity of the interphase modifier is typically from about 0.7 to about 200 centistokes (“cs”), in some embodiments from about 1 to about 100 cs, and in some embodiments, from about 1.5 to about 80 cs, determined at 40° C. In addition, the interphase modifier is also typically hydrophobic so that it has an affinity for the polymer toughening additive, resulting in a change in the interfacial tension between the renewable polyester and the toughening additive. By reducing physical forces at the interfaces between the polyester and the toughening additive, it is believed that the low viscosity, hydrophobic nature of the modifier can help facilitate debonding from the polyester matrix. As used herein, the term “hydrophobic” typically refers to a material having a contact angle of water in air of about 40° or more, and in some cases, about 60° or more. In contrast, the term “hydrophilic” typically refers to a material having a contact angle of water in air of less than about 40°. One suitable test for measuring the contact angle is ASTM D5725-99 (2008).

Suitable hydrophobic, low viscosity interphase modifiers may include, for instance, silicones, silicone-polyether copolymers, aliphatic polyesters, aromatic polyesters, alkylene glycols (e.g., ethylene glycol, diethylene glycol, triethylene glycol, tetraethylene glycol, propylene glycol, polyethylene glycol, polypropylene glycol, polybutylene glycol, etc.), alkane diols (e.g., 1,3-propanediol, 2,2-dimethyl-1,3-propanediol, 1,3-butanediol, 1,4-butanediol, 1,5-pentanediol, 1,6-hexanediol, 2,2,4-trimethyl-1,6 hexanediol, 1,3-cyclohexanedimethanol, 1,4-cyclohexanedimethanol, 2,2,4,4-tetramethyl-1,3-cyclobutanediol, etc.), amine oxides (e.g., octyldimethylamine oxide), fatty acid esters, etc. One particularly suitable interphase modifier is polyether polyol, such as commercially available under the trade name PLURIOL® WI from BASF Corp. Another suitable modifier is a partially renewable ester, such as commercially available under the trade name HALLGREEN® IM from Hallstar.

Although the actual amount may vary, the interphase modifier is typically employed in an amount of from about 0.1 wt. % to about 20 wt. %, in some embodiments from about 0.5 wt. % to about 15 wt. %, and in some embodiments, from about 1 wt. % to about 10 wt. % of the thermoplastic composition, based on the weight of the renewable polyesters employed in the composition. The concentration of the interphase modifier in the entire thermoplastic composition may likewise constitute from about 0.05 wt. % to about 20 wt. %, in some embodiments from about 0.1 wt. % to about 15 wt. %, and in some embodiments, from about 0.5 wt. % to about 10 wt. %.

When employed in the amounts noted above, the interphase modifier has a character that enables it to readily migrate to the interfacial surface of the polymers and facilitate debonding without disrupting the overall melt properties of the thermoplastic composition. For example, the interphase modifier does not typically have a plasticizing effect on the polymer by reducing its glass transition temperature. Quite to the contrary, the present inventors have discovered that the glass transition temperature of the thermoplastic composition may be substantially the same as the initial renewable polyester. In this regard, the ratio of the glass temperature of the composition to that of the polyester is typically from about 0.7 to about 1.3, in some embodiments from about 0.8 to about 1.2, and in some embodiments, from about 0.9 to about 1.1. The thermoplastic composition may, for example, have a glass transition temperature of from about 35° C. to about 80° C., in some embodiments from about 40° C. to about 80° C., and in some embodiments, from about 50° C. to about 65° C. The melt flow rate of the thermoplastic composition may also be similar to that of the renewable polyester. For example, the melt flow rate of the composition (on a dry basis) may be from about 0.1 to about 70 grams per 10 minutes, in some embodiments from about 0.5 to about 50 grams per 10 minutes, and in some embodiments, from about 5 to about 25 grams per 10 minutes, determined at a load of 2160 grams and at a temperature of 190° C.

D. Compatibilizer

As indicated above, the polymeric toughening additive is generally selected so that it has a solubility parameter relatively close to that of the renewable polyester. Among other things, this can enhance the compatibility of the phases and improve the overall distribution of the discrete domains within the continuous phase. Nevertheless, in certain embodiments, a compatibilizer may optionally be employed to further enhance the compatibility between the renewable polyester and the polymeric toughening additive. This may be particularly desirable when the polymeric toughening additive possesses a polar moiety, such as polyurethanes, acrylic resins, etc. When employed, the compatibilizers typically constitute from about 0.5 wt. % to about 20 wt. %, in some embodiments from about 1 wt. % to about 15 wt. %, and in some embodiments, from about 1.5 wt. % to about 10 wt. % of the thermoplastic composition. One example of a suitable compatibilizer is a functionalized polyolefin. The polar component may, for example, be provided by one or more functional groups and the non-polar component may be provided by an olefin. The olefin component of the compatibilizer may generally be formed from any linear or branched α-olefin monomer, oligomer, or polymer (including copolymers) derived from an olefin monomer, such as described above.

The functional group of the compatibilizer may be any group that provides a polar segment to the molecule. Particularly suitable functional groups are maleic anhydride, maleic acid, fumaric acid, maleimide, maleic acid hydrazide, a reaction product of maleic anhydride and diamine, methylnadic anhydride, dichloromaleic anhydride, maleic acid amide, etc. Maleic anhydride modified polyolefins are particularly suitable for use in the present invention. Such modified polyolefins are typically formed by grafting maleic anhydride onto a polymeric backbone material. Such maleated polyolefins are available from E. I. du Pont de Nemours and Company under the designation Fusabond®, such as the P Series (chemically modified polypropylene), E Series (chemically modified polyethylene), C Series (chemically modified ethylene vinyl acetate), A Series (chemically modified ethylene acrylate copolymers or terpolymers), or N Series (chemically modified ethylene-propylene, ethylene-propylene diene monomer (“EPDM”) or ethylene-octene). Alternatively, maleated polyolefins are also available from Chemtura Corp. under the designation Polybond® and Eastman Chemical Company under the designation Eastman G series.

In certain embodiments, the compatibilizer may also be reactive. One example of such a reactive compatibilizer is a polyepoxide modifier that contains, on average, at least two oxirane rings per molecule. Without intending to be limited by theory, it is believed that such polyepoxide molecules can induce reaction of the renewable polyester under certain conditions, thereby improving its melt strength without significantly reducing glass transition temperature. The reaction may involve chain extension, side chain branching, grafting, copolymer formation, etc. Chain extension, for instance, may occur through a variety of different reaction pathways. For instance, the modifier may enable a nucleophilic ring-opening reaction via a carboxyl terminal group of the renewable polyester (esterification) or via a hydroxyl group (etherification). Oxazoline side reactions may likewise occur to form esteramide moieties. Through such reactions, the molecular weight of the renewable polyester may be increased to counteract the degradation often observed during melt processing. While it is desirable to induce a reaction with the renewable polyester as described above, the present inventors have discovered that too much of a reaction can lead to crosslinking between polyester backbones. If such crosslinking is allowed to proceed to a significant extent, the resulting polymer blend can become brittle and difficult to mold into a material with the desired strength and elongation properties.

In this regard, the present inventors have discovered that polyepoxide modifiers having a relatively low epoxy functionality are particularly effective, which may be quantified by its “epoxy equivalent weight.” The epoxy equivalent weight reflects the amount of resin that contains one molecule of an epoxy group, and it may be calculated by dividing the number average molecular weight of the modifier by the number of epoxy groups in the molecule. The polyepoxide modifier of the present invention typically has a number average molecular weight from about 7,500 to about 250,000 grams per mole, in some embodiments from about 15,000 to about 150,000 grams per mole, and in some embodiments, from about 20,000 to 100,000 grams per mole, with a polydispersity index typically ranging from 2.5 to 7. The polyepoxide modifier may contain less than 50, in some embodiments from 5 to 45, and in some embodiments, from 15 to 40 epoxy groups. In turn, the epoxy equivalent weight may be less than about 15,000 grams per mole, in some embodiments from about 200 to about 10,000 grams per mole, and in some embodiments, from about 500 to about 7,000 grams per mole.

The polyepoxide may be a linear or branched, homopolymer or copolymer (e.g., random, graft, block, etc.) containing terminal epoxy groups, skeletal oxirane units, and/or pendent epoxy groups. The monomers employed to form such polyepoxides may vary. In one particular embodiment, for example, the polyepoxide modifier contains at least one epoxy-functional (meth)acrylic monomeric component. As used herein, the term “(meth)acrylic” includes acrylic and methacrylic monomers, as well as salts or esters thereof, such as acrylate and methacrylate monomers. For example, suitable epoxy-functional (meth)acrylic monomers may include, but are not limited to, those containing 1,2-epoxy groups, such as glycidyl acrylate and glycidyl methacrylate. Other suitable epoxy-functional monomers include allyl glycidyl ether, glycidyl ethacrylate, and glycidyl itoconate.

The polyepoxide typically has a relatively high molecular weight, as indicated above, so that it can not only result in chain extension of the renewable polyester, but also help to achieve the desired blend morphology. The resulting melt flow rate of the polymer is thus typically within a range of from about 10 to about 200 grams per 10 minutes, in some embodiments from about 40 to about 150 grams per 10 minutes, and in some embodiments, from about 60 to about 120 grams per 10 minutes, determined at a load of 2160 grams and at a temperature of 190° C.

If desired, additional monomers may also be employed in the polyepoxide to help achieve the desired molecular weight. Such monomers may vary and include, for example, ester monomers, (meth)acrylic monomers, olefin monomers, amide monomers, etc. In one particular embodiment, for example, the polyepoxide modifier includes at least one linear or branched α-olefin monomer, such as those having from 2 to 20 carbon atoms and preferably from 2 to 8 carbon atoms. Specific examples include ethylene, propylene, 1-butene; 3-methyl-1-butene; 3,3-dimethyl-1-butene; 1-pentene; 1-pentene with one or more methyl, ethyl or propyl substituents; 1-hexene with one or more methyl, ethyl or propyl substituents; 1-heptene with one or more methyl, ethyl or propyl substituents; 1-octene with one or more methyl, ethyl or propyl substituents; 1-nonene with one or more methyl, ethyl or propyl substituents; ethyl, methyl or dimethyl-substituted 1-decene; 1-dodecene; and styrene. Particularly desired α-olefin comonomers are ethylene and propylene.

Another suitable monomer may include a (meth)acrylic monomer that is not epoxy-functional. Examples of such (meth)acrylic monomers may include methyl acrylate, ethyl acrylate, n-propyl acrylate, i-propyl acrylate, n-butyl acrylate, s-butyl acrylate, i-butyl acrylate, t-butyl acrylate, n-amyl acrylate, i-amyl acrylate, isobornyl acrylate, n-hexyl acrylate, 2-ethylbutyl acrylate, 2-ethylhexyl acrylate, n-octyl acrylate, n-decyl acrylate, methylcyclohexyl acrylate, cyclopentyl acrylate, cyclohexyl acrylate, methyl methacrylate, ethyl methacrylate, 2-hydroxyethyl methacrylate, n-propyl methacrylate, n-butyl methacrylate, i-propyl methacrylate, i-butyl methacrylate, n-amyl methacrylate, n-hexyl methacrylate, i-amyl methacrylate, s-butyl-methacrylate, t-butyl methacrylate, 2-ethylbutyl methacrylate, methylcyclohexyl methacrylate, cinnamyl methacrylate, crotyl methacrylate, cyclohexyl methacrylate, cyclopentyl methacrylate, 2-ethoxyethyl methacrylate, isobornyl methacrylate, etc., as well as combinations thereof.

In one particularly desirable embodiment of the present invention, the polyepoxide modifier is a terpolymer formed from an epoxy-functional (meth)acrylic monomeric component, α-olefin monomeric component, and non-epoxy functional (meth)acrylic monomeric component. For example, the polyepoxide modifier may be poly(ethylene-co-methylacrylate-co-glycidyl methacrylate), which has the following structure:

wherein, x, y, and z are 1 or greater.

The epoxy functional monomer may be formed into a polymer using a variety of known techniques. For example, a monomer containing polar functional groups may be grafted onto a polymer backbone to form a graft copolymer. Such grafting techniques are well known in the art and described, for instance, in U.S. Pat. No. 5,179,164, which is incorporated herein in its entirety by reference thereto for all purposes. In other embodiments, a monomer containing epoxy functional groups may be copolymerized with a monomer to form a block or random copolymer using known free radical polymerization techniques, such as high pressure reactions, Ziegler-Natta catalyst reaction systems, single site catalyst (e.g., metallocene) reaction systems, etc.

The relative portion of the monomeric component(s) may be selected to achieve a balance between epoxy-reactivity and melt flow rate. More particularly, high epoxy monomer contents can result in good reactivity with the renewable polyester, but too high of a content may reduce the melt flow rate to such an extent that the polyepoxide modifier adversely impacts the melt strength of the polymer blend. Thus, in most embodiments, the epoxy-functional (meth)acrylic monomer(s) constitute from about 1 wt. % to about 25 wt. %, in some embodiments from about 2 wt. % to about 20 wt. %, and in some embodiments, from about 4 wt. % to about 15 wt. % of the copolymer. The α-olefin monomer(s) may likewise constitute from about 55 wt. % to about 95 wt. %, in some embodiments from about 60 wt. % to about 90 wt. %, and in some embodiments, from about 65 wt. % to about 85 wt. % of the copolymer. When employed, other monomeric components (e.g., non-epoxy functional (meth)acrylic monomers) may constitute from about 5 wt. % to about 35 wt. %, in some embodiments from about 8 wt. % to about 30 wt. %, and in some embodiments, from about 10 wt. % to about 25 wt. % of the copolymer. One specific example of a suitable polyepoxide modifier that may be used in the present invention is commercially available from Arkema under the name LOTADER® AX8950 or AX8900. LOTADER® AX8950, for instance, has a melt flow rate of 70 to 100 g/10 min and has a glycidyl methacrylate monomer content of 7 wt. % to 11 wt. %, a methyl acrylate monomer content of 13 wt. % to 17 wt. %, and an ethylene monomer content of 72 wt. % to 80 wt. %.

In addition to controlling the type and relative content of the monomers used to form the polyepoxide modifier, the overall weight percentage may also be controlled to achieve the desired benefits. For example, if the modification level is too low, the desired increase in melt strength and mechanical properties may not be achieved. The present inventors have also discovered, however, that if the modification level is too high, molding may be restricted due to strong molecular interactions (e.g., crosslinking) and physical network formation by the epoxy functional groups. Thus, the polyepoxide modifier is typically employed in an amount of from about 0.05 wt. % to about 10 wt. %, in some embodiments from about 0.1 wt. % to about 8 wt. %, in some embodiments from about 0.5 wt. % to about 5 wt. %, and in some embodiments, from about 1 wt. % to about 3 wt. %, based on the weight of the renewable polyesters employed in the composition. The polyepoxide modifier may also constitute from about 0.05 wt. % to about 10 wt. %, in some embodiments from about 0.05 wt. % to about 8 wt. %, in some embodiments from about 0.1 wt. % to about 5 wt. %, and in some embodiments, from about 0.5 wt. % to about 3 wt. %, based on the total weight of the composition.

In addition to polyepoxides, other reactive compatibilizers may also be employed in the present invention, such as oxazoline-functionalized polymers, cyanide-functionalized polymers, etc. When employed, such reactive compatibilizers may be employed within the concentrations noted above for the polyepoxide modifier. In one particular embodiment, an oxazoline-grafted polyolefin may be employed that is a polyolefin grafted with an oxazoline ring-containing monomer. The oxazoline may include a 2-oxazoline, such as 2-vinyl-2-oxazoline (e.g., 2-isopropenyl-2-oxazoline), 2-fatty-alkyl-2-oxazoline (e.g., obtainable from the ethanolamide of oleic acid, linoleic acid, palmitoleic acid, gadoleic acid, erucic acid and/or arachidonic acid) and combinations thereof. In another embodiment, the oxazoline may be selected from ricinoloxazoline maleinate, undecyl-2-oxazoline, soya-2-oxazoline, ricinus-2-oxazoline and combinations thereof, for example. In yet another embodiment, the oxazoline is selected from 2-isopropenyl-2-oxazoline, 2-isopropenyl-4,4-dimethyl-2-oxazoline and combinations thereof.

E. Other Components

One beneficial aspect of the present invention is that good mechanical properties may be provided without the need for various conventional additives, such as blowing agents (e.g., chlorofluorocarbons, hydrochlorofluorocarbons, hydrocarbons, carbon dioxide, etc.) and plasticizers (e.g., solid or semi-solid polyethylene glycol). In fact, the thermoplastic composition may be substantially free of blowing agents and/or plasticizers. For example, blowing agents and/or plasticizers may be present in an amount of no more than about 1 wt. %, in some embodiments no more than about 0.5 wt. %, and in some embodiments, from about 0.001 wt. % to about 0.2 wt. % of the thermoplastic composition. Further, due to its stress whitening properties, as described in more detail below, the resulting composition may achieve an opaque color (e.g., white) without the need for conventional pigments, such as titanium dioxide. In certain embodiments, for example, pigments may be present in an amount of no more than about 1 wt. %, in some embodiments no more than about 0.5 wt. %, and in some embodiments, from about 0.001 wt. % to about 0.2 wt. % of the thermoplastic composition. Of course, a wide variety of ingredients may be utilized in the composition for a variety of different reasons. For instance, materials that may be used include, without limitation, catalysts, antioxidants, stabilizers, surfactants, waxes, solid solvents, fillers, nucleating agents (e.g., calcium carbonate, etc.), particulates, and other materials added to enhance the processability of the thermoplastic composition.

II. Formation of Precursor Material

As indicated above, the thermoplastic composition of the present invention is generally formed by cold drawing a precursor material that contains the rigid renewable polyester, polymeric toughening additive, as well as other optional components. To form the precursor material, the components are typically blended together using any of a variety of known techniques. In one embodiment, for example, the components may be supplied separately or in combination. For instance, the components may first be dry mixed together to form an essentially homogeneous dry mixture, and they may likewise be supplied either simultaneously or in sequence to a melt processing device that dispersively blends the materials. Batch and/or continuous melt processing techniques may be employed. For example, a mixer/kneader, Banbury mixer, Farrel continuous mixer, single-screw extruder, twin-screw extruder, roll mill, etc., may be utilized to blend and melt process the materials. Particularly suitable melt processing devices may be a co-rotating, twin-screw extruder (e.g., ZSK-30 extruder available from Wemer & Pfleiderer Corporation of Ramsey, N.J. or a Thermo Prism™ USALAB 16 extruder available from Thermo Electron Corp., Stone, England). Such extruders may include feeding and venting ports and provide high intensity distributive and dispersive mixing. For example, the components may be fed to the same or different feeding ports of the twin-screw extruder and melt blended to form a substantially homogeneous melted mixture. If desired, other additives may also be injected into the polymer melt and/or separately fed into the extruder at a different point along its length.

Regardless of the particular processing technique chosen, the resulting melt blended material typically contains domains of the toughening additive with an axial dimension of a domain (e.g., length) of from about 0.05 μm to about 30 μm, in some embodiments from about 0.1 μm to about 25 μm, in some embodiments from about 0.5 μm to about 20 μm, and in some embodiments from about 1 μm to about 10 μm. When employed the polyepoxide modifier may also be in the form of discrete domains distributed throughout the continuous polyester matrix. These “secondary” domains may have a variety of different shapes, such as elliptical, spherical, cylindrical, etc. Regardless of the shape, however, the size of an individual secondary domain, after blending, is small to provide an increased surface area for reaction with the renewable polyester. For example, the size of a secondary domain (e.g., length) typically ranges from about 10 to about 1000 nanometers, in some embodiments from about 20 to about 800 nanometers, in some embodiments from about 40 to about 600 nanometers, and in some embodiments from about 50 to about 400 nanometers. As noted above, the toughening additive also forms discrete domains within the polyester matrix, which are considered in the “primary” domains of the composition. Of course, it should be also understood that domains may be formed by a combination of the polyepoxide, toughening additive, and/or other components of the blend.

The degree of shear/pressure and heat may be controlled to ensure sufficient dispersion, but not so high as to adversely reduce the size of the discrete domains so that they are incapable of achieving the desired toughness and elongation. For example, blending typically occurs at a temperature of from about 180° C. to about 260° C., in some embodiments from about 185° C. to about 250° C., and in some embodiments, from about 190° C. to about 240° C. Likewise, the apparent shear rate during melt processing may range from about 10 seconds⁻¹ to about 3000 seconds⁻¹, in some embodiments from about 50 seconds⁻¹ to about 2000 seconds⁻¹, and in some embodiments, from about 100 seconds⁻¹ to about 1200 seconds⁻¹. The apparent shear rate is equal to 4Q/πR³, where Q is the volumetric flow rate (“m³/s”) of the polymer melt and R is the radius (“m”) of the capillary (e.g., extruder die) through which the melted polymer flows. Of course, other variables, such as the residence time during melt processing, which is inversely proportional to throughput rate, may also be controlled to achieve the desired degree of homogeneity.

To achieve the desired shear conditions (e.g., rate, residence time, shear rate, melt processing temperature, etc.), the speed of the extruder screw(s) may be selected with a certain range. Generally, an increase in product temperature is observed with increasing screw speed due to the additional mechanical energy input into the system. For example, the screw speed may range from about 50 to about 300 revolutions per minute (“rpm”), in some embodiments from about 70 to about 500 rpm, and in some embodiments, from about 100 to about 300 rpm. This may result in a temperature that is sufficient high to disperse the toughening additive without adversely impacting the size of the resulting domains. The melt shear rate, and in turn the degree to which the polymers are dispersed, may also be increased through the use of one or more distributive and/or dispersive mixing elements within the mixing section of the extruder. Suitable distributive mixers for single screw extruders may include, for instance, Saxon, Dulmage, Cavity Transfer mixers, etc. Likewise, suitable dispersive mixers may include Blister ring, Leroy/Maddock, CRD mixers, etc. As is well known in the art, the mixing may be further improved by using pins in the barrel that create a folding and reorientation of the polymer melt, such as those used in Buss Kneader extruders, Cavity Transfer mixers, and Vortex Intermeshing Pin (VIP) mixers.

Once blended, the resulting material may be formed into a precursor material using any of a variety of known techniques, such as extrusion, profile extrusion, film casting, blowing, thermoforming, injection molding, compression molding, rotational molding, etc. In one embodiment, for example, the precursor material is in the form of a sheet having a thickness of from about 1 to about 5000 micrometers, in some embodiments from about 2 to about 4000 micrometers, in some embodiments from about 5 to about 2500 micrometers, and in some embodiments, from about 10 to about 500 micrometers.

Regardless of the particular nature of the precursor material, a voided network structure is introduced by stretching it at a temperature below the glass transition temperature of the renewable polyester. Stretching may occur in the longitudinal direction (e.g., machine direction), transverse direction (e.g., cross-machine direction), or a combination thereof. Although not required, the precursor material may be stretched in-line without having to remove it for separate processing. Various stretching techniques may be employed, such as tensile frame drawing, biaxial drawing, multi-axial drawing, profile drawing, cold air drawing, vacuum drawing, etc. For example, the precursor material may be drawn in a longitudinal direction by rolls rotating at different speeds of rotation.

The degree of stretching is generally selected in the present invention to ensure that the desired voided network is achieved, but not to such an extent that the precursor material necks to a significant extent. In this regard, the precursor material is typically stretched (e.g., in the machine direction) to a draw ratio of from about 1.1 to about 3.0, in some embodiments from about 1.2 to about 2.0, and in some embodiments, from about 1.3 to about 1.8. The draw ratio may be determined by dividing the length of the stretched material by its length before stretching. The draw rate may also vary to help achieve the desired properties, such as within the range of from about 5% to about 1500% per minute of deformation, in some embodiments from about 10% to about 1000% per minute of deformation, and in some embodiments, from about 100% to about 850% per minute of deformation. The precursor material is generally kept at a temperature below the glass temperature of the renewable polyester during stretching. Among other things, this helps to ensure that the polyester chains are not altered to such an extent that the voided network becomes unstable. Typically, the precursor material is stretched at a temperature that is at least about 10° C., in some embodiments at least about 20° C., and in some embodiments, at least about 30° C. below then glass transition temperature. For example, the precursor material may be stretched at a temperature of from about 0° C. to about 50° C., in some embodiments from about 15° C. to about 40° C., and in some embodiments, from about 20° C. to about 30° C. If desired, the precursor material is stretched without the application of external heat (e.g., heated rolls).

Cold drawing in the manner described above generally results in the formation of voids that have an axial dimension in the direction of stretching (e.g., longitudinal or machine direction) that is relatively small. For example, in one embodiment, the axial dimension of the voids may be about 5 micrometers or less, in some embodiments about 2 micrometers or less, and in some embodiments, from about 25 nanometers to about 1 micrometer. In certain cases, the voids may be “micro-voids” in the sense that at least one dimension of such voids has a size of about 1 micrometer or more. For example, such micro-voids may have a dimension in a direction orthogonal to the axial dimension (i.e., transverse or cross-machine direction) that is about 1 micrometer or more, in some embodiments about 1.5 micrometers or more, and in some embodiments, from about 2 micrometers to about 5 micrometers. This may result in an aspect ratio for the micro-voids (the ratio of the axial dimension to the dimension orthogonal to the axial dimension) of from about 0.1 to about 1, in some embodiments from about 0.2 to about 0.9, and in some embodiments, from about 0.3 to about 0.8. Likewise, “nano-voids” may also be present, either alone or in conjunction with the micro-voids. Each dimension of the nano-voids is typically less than about 1 micrometer, and in some embodiments, from about 25 to about 500 nanometers.

In addition to forming a voided network as described above, drawing can also significantly increase the axial dimension of the primary domains so that they have a generally linear, elongated shape. For example, the elongated domains may have an axial dimension that is about 10% or more, in some embodiments from about 20% to about 500%, and in some embodiments, from about 50% to about 250% greater than the axial dimension of the domains prior to drawing. The axial dimension after drawing may, for instance, range from about 1 μm to about 400 μm, in some embodiments from about 5 μm to about 200 μm, and in some embodiments from about 10 μm to about 150 μm. The domains may also be relatively thin and thus have a small dimension in a direction orthogonal to the axial dimension (i.e., cross-sectional dimension). For instance, the cross-sectional dimension may be from about 0.02 to about 75 micrometers, in some embodiments from about 0.1 to about 40 micrometers, and in some embodiments, from 0.4 to about 20 micrometers in length. This may result in an aspect ratio for the domains (the ratio of the axial dimension to a dimension orthogonal to the axial dimension) of from about 2 to about 150, in some embodiments from about 3 to about 100, and in some embodiments, from about 4 to about 50.

As a result of the voided and elongated domain structure obtained from cold drawing, the present inventors have discovered that the resulting composition can expand uniformly in volume when drawn in longitudinal direction, which is reflected by a low “Poisson coefficient”, as determined according to the following equation:

Poisson coefficient=−E _(transverse) /E _(longitudinal)

where E_(transverse) is the transverse deformation of the material and E a is the longitudinal deformation of the material. More particularly, the Poisson coefficient of the material can be approximately 0 or even negative. For example, the Poisson coefficient may be about 0.1 or less, in some embodiments about 0.08 or less, and in some embodiments, from about −0.1 to about 0.04. When the Poisson coefficient is zero, there is no contraction in transverse direction when the material is expanded in the longitudinal direction. When the Poisson coefficient is negative, the transverse or lateral dimensions of the material are also expanding when the material is drawn in the longitudinal direction. Materials having a negative Poisson coefficient can thus exhibit an increase in width when stretched in the longitudinal direction, which can result in increased energy absorption in the cross direction.

Even at the very low densities achieved by the present invention, the resulting thermoplastic composition still has excellent mechanical properties due to its unique structure and morphology. In fact, the thermoplastic composition may possess certain properties, such as impact strength, that are significantly higher than conventional compositions. For example, the thermoplastic composition may possess an Izod notched impact strength of about 1 Joules per centimeter (“J/cm”) or more, in some embodiments about 3 J/cm or more, and in some embodiments, from about 5 J/cm to about 15 J/cm, measured at 23° C. according ASTM D256-10 (Method A). The tensile elongation at break may also be relatively high, such as about 40% or more, in some embodiments about 60% or more, and in some embodiments, from about 70% to about 300%. While achieving a very high degree of impact strength and tensile elongation, the present inventors have discovered that other mechanical properties are not adversely affected. For example, the composition may exhibit a peak stress of from about 10 to about 65 Megapascals (“MPa”), in some embodiments from about 15 to about 55 MPa, and in some embodiments, from about 25 to about 50 MPa; a break stress of from about 10 to about 65 MPa, in some embodiments from about 15 to about 60 MPa, and in some embodiments, from about 20 to about 55 MPa; and/or a tensile modulus of from about 50 to about 3800 MPa, in some embodiments from about 100 MPa to about 1500 MPa, and in some embodiments, from about 200 MPa to about 1000 MPa. The tensile properties may be determined in accordance with ASTM D638-10 at 23° C.

Another benefit of the present invention is that the voided structure may have a higher surface roughness than the precursor material, which can improve tactile feel and softness of the resulting article. For example, the voided structure may have an average surface roughness of about 0.2 μm or more, in some embodiments about 0.3 μm or more, and in some embodiments, from about 0.5 to about 1.5 μm. The average surface roughness may be determined from the surface topography profile as described below, and is generally calculated as the arithmetic average of the absolute values of the roughness profile values. Such measurements and calculations may be conducted in accordance with ISO 25178.

III. Shaped Articles

Due to its unique and beneficial properties, the cold drawn thermoplastic composition of the present invention is well suited for use in shaped articles, and particularly those having a relatively small thickness. For example, the article may have a thickness of about 100 micrometers to about 50 millimeters, in some embodiments from about 200 micrometers to about 10 millimeters, in some embodiments from about 400 micrometers to about 5 millimeters, and in some embodiments, from about 500 micrometers to about 2 millimeters.

The shaped article may be formed using any of a variety of techniques known in the art, such as profile extrusion, extrusion blow molding, injection molding, rotational molding, compression molding, etc., as well as combinations of the foregoing. Regardless of the process selected, the cold drawn composition may be used alone to form the article, or in combination with other polymeric components to form a shaped articles. For example, the composition can be profile extruded as a core while other polymer(s) can be extruded as a “skin” or external layer. In another embodiment, other polymer(s) may be injected or transferred into a mold during an injection molding process to form a skin layer around a core. Examples of machines suitable for co-injection, sandwich or two-component molding include machines produced by Presma Corp., Northeast Mold & Plastics, Inc. Although not required, the core of the shaped article is typically formed from the cold drawn composition of the present invention and the skin layer is typically formed from a different polymer (e.g., polyolefins, polyesters, polyamides, etc.) that enhances surface and bulk and bonding properties for intended use.

Referring to FIG. 1, for example, one particular embodiment of a single-component injection molding apparatus or tool 10 that may be employed in the present invention is shown in more detail. In this embodiment, the apparatus 10 includes a first mold base 12 and a second mold base 14, which together define an article or component-defining mold cavity 16. Each of the mold bases 12 and 14 includes one or more cooling lines 18 through which a cooling liquid such as water flows to cool the apparatus 10 during use. The molding apparatus 10 also includes a resin flow path that extends from an outer exterior surface 20 of the first mold half 12 through a sprue 22 to the article-defining mold cavity 16. The resin flow path may also include a runner and a gate, both of which are not shown for purposes of simplicity. The molding apparatus 10 also includes one or more ejector pins 24 slidably secured within the second mold half 14 that helps to define the article-defining cavity 16 in the closed position of the apparatus 10, as indicated in FIG. 1. The ejector pin 24 operates in a well-known fashion to remove a molded article or component from the article-defining cavity 16 in the open position of the molding apparatus 10.

The cold drawn composition may be directly injected into the molding apparatus 10 using techniques known in the art. For example, the composition may be supplied in the form of a sheet to a feed hopper attached to a barrel that contains a rotating screw (not shown). As the screw rotates, the sheet is moved forward and undergoes extreme pressure and friction, which generates heat to melt the polymer. Electric heater bands (not shown) attached to the outside of the barrel may also assist in the heating and temperature control during the melting process. For example, the bands may be heated to a temperature of from about 200° C. to about 260° C., in some embodiments from about 230° C. to about 255° C., and in some embodiments, from about 240° C. to about 250° C. Upon entering the molding cavity 16, the composition is solidified by the cooling liquid flowing through the lines 18. The cooling liquid may, for example, be at a temperature (the “molding temperature”) of from about 5° C. to about 50° C., in some embodiments from about 10° C. to about 40° C., and in some embodiments, from about 15° C. to about 30° C.

If desired, the molded article may also be annealed to help ensure that it retains the desired shape. Annealing typically occurs at temperatures above the glass transition temperature of the renewable polyester, such as at temperatures of from about 65° to about 120° C., in some embodiments from about 70° C. to about 110° C., and in some embodiments, from about 80° C. to about 100° C. The articles may also be surface treated using any of a variety of known techniques to improve its properties. For example, high energy beams (e.g., plasma, x-rays, e-beam, etc.) may be used to remove or reduce any skin layers that form on the molded article, to change the surface polarity, embrittle a surface layer, etc. If desired, such surface treatment may alternatively be used prior to molding and before and/or after cold drawing of the precursor material.

The resulting shaped articles may have a variety of different sizes and configurations. For instance, the article may be used to form dispensers (e.g., for paper towels), packaging materials (e.g., food packaging, medical packaging, etc.), medical devices, such as surgical instruments (e.g., scalpels, scissors, retractors, suction tubes, probes, etc.); implants (e.g., bone plates, prosthetics, plates, screws, etc.); containers or bottles; and so forth. The article may also be used to form various parts used in “personal care” applications. For instance, in one particular embodiment, the article is used to form a wet wipe container. The configuration of the container may vary as is known in the art, such as described in U.S. Pat. No. 5,687,875 to Watts, et al.; U.S. Pat. No. 6,568,625 to Faulks, et al.; U.S. Pat. No. 6,158,614 to Haines, et al.; U.S. Pat. No. 3,973,695 to Ames; U.S. Pat. No. 6,523,690 to Buck, et al.; and U.S. Pat. No. 6,766,919 to Huana. et al., which are incorporated herein in their entirety by reference thereto for all purposes. Wipes for use with the container, e.g., wet wipes, may be arranged in any manner that provides convenient and reliable dispensing and that assists the wet wipes in not becoming overly dry. For example, the wet wipes may be arranged in the container as a plurality of individual wipes in a stacked configuration to provide a stack of wet wipes that may or may not be individually folded. The wet wipes can be individual wet wipes which are folded in a c-fold configuration, z-fold configuration, connected to adjacent wipes by a weakened line or other non-interfolded configurations as are known to those skilled in the art. Alternatively, the individual wet wipes can be interfolded such that the leading and trailing end edges of successive wipes in the stacked configuration overlap. In each of these non-interfolded and interfolded configurations, the leading end edge of the following wet wipe is loosened from the stack by the trailing end edge of the leading wet wipe as the leading wet wipe is removed by the user from the dispenser or package. For example, representative wet wipes for use with the invention are described in U.S. Pat. No. 6,585,131 to Huang. et al. and U.S. Pat. No. 6,905,748 to Sosalla, which are incorporated herein in their entirety by reference thereto for all purposes.

The present invention may be better understood with reference to the following examples.

Test Methods Melt Flow Rate:

The melt flow rate (“MFR”) is the weight of a polymer (in grams) forced through an extrusion rheometer orifice (0.0825-inch diameter) when subjected to a load of 2160 grams in 10 minutes, typically at 190° C. or 230° C. Unless otherwise indicated, melt flow rate is measured in accordance with ASTM Test Method D1239 with a Tinius Olsen Extrusion Plastometer.

Thermal Properties:

The glass transition temperature (T_(g)) may be determined by dynamic mechanical analysis (DMA) in accordance with ASTM E1640-09. A Q800 instrument from TA Instruments may be used. The experimental runs may be executed in tension/tension geometry, in a temperature sweep mode in the range from −120° C. to 150° C. with a heating rate of 3° C./min. The strain amplitude frequency may be kept constant (2 Hz) during the test. Three (3) independent samples may be tested to get an average glass transition temperature, which is defined by the peak value of the tan δ curve, wherein tan δ is defined as the ratio of the loss modulus to the storage modulus (tan δ=E″/E′).

The melting temperature may be determined by differential scanning calorimetry (DSC). The differential scanning calorimeter may be a DSC Q100 Differential Scanning Calorimeter, which was outfitted with a liquid nitrogen cooling accessory and with a UNIVERSAL ANALYSIS 2000 (version 4.6.6) analysis software program, both of which are available from T.A. Instruments Inc. of New Castle, Del. To avoid directly handling the samples, tweezers or other tools are used. The samples are placed into an aluminum pan and weighed to an accuracy of 0.01 milligram on an analytical balance. A lid is crimped over the material sample onto the pan. Typically, the resin pellets are placed directly in the weighing pan.

The differential scanning calorimeter is calibrated using an indium metal standard and a baseline correction is performed, as described in the operating manual for the differential scanning calorimeter. A material sample is placed into the test chamber of the differential scanning calorimeter for testing, and an empty pan is used as a reference. All testing is run with a 55-cubic centimeter per minute nitrogen (industrial grade) purge on the test chamber. For resin pellet samples, the heating and cooling program is a 2-cycle test that began with an equilibration of the chamber to −30° C., followed by a first heating period at a heating rate of 10° C. per minute to a temperature of 200° C., followed by equilibration of the sample at 200° C. for 3 minutes, followed by a first cooling period at a cooling rate of 10° C. per minute to a temperature of −30° C., followed by equilibration of the sample at −30° C. for 3 minutes, and then a second heating period at a heating rate of 10° C. per minute to a temperature of 200° C. All testing is run with a 55-cubic centimeter per minute nitrogen (industrial grade) purge on the test chamber.

The results are evaluated using the UNIVERSAL ANALYSIS 2000 analysis software program, which identified and quantified the glass transition temperature (T_(g)) of inflection, the endothermic and exothermic peaks, and the areas under the peaks on the DSC plots. The glass transition temperature is identified as the region on the plot-line where a distinct change in slope occurred, and the melting temperature is determined using an automatic inflection calculation.

Notched Izod Impact Strength:

Notched Impact strength of injection molded Izod bars were determined by following ASTM D256-10 Method A (Standard Test Methods for Determining the Izod Pendulum Impact Resistance of Plastics). Izod bars were conditioned for 40+ hours at 23° C.±2° C. at 50%±10% relative humidity before testing in the same conditions. The pendulum had a capacity of 2 ft·lbs. Injection molded Izod test specimens had a width 12.70±0.20 mm and thickness of 3.2±0.05 mm.

Tensile Properties:

Modulus was determined utilizing a MTS 810 hydraulic tensile frame to pull injection molded Type I dog bones as described in ASTM D638-10. Specimens were conditioned at 23° C.±2° C. and 50%±10% relative humidity for not less than 40 hours. Test conditions were at 23° C.±2° C. and 50%±10% relative humidity. Tensile frame grips were at a nominal gage length of 115 mm. Specimens were pulled at a rate of 50 mm/min (87.7%. min deformation). Five (5) specimens were tested for each composition. A computer program called TestWorks 4 was used to collect data during testing and to generate a stress versus strain curve from which the average modulus of five specimens was determined.

Peak stress, break stress, elongation at break, and energy per volume at break were determined using a MTS Synergie 200 tensile frame to pull injection molded Type V dog bones at described in ASTM D638-10. Specimens were conditioned at 23° C.±2° C. at 50%±10% relative humidity for not less than 40 hours. Test conditions were at 23° C.±2° C. at 20%±10% relative humidity. Tensile frame grips were at a nominal gage length of 25.4 mm. Specimens were pulled at a rate of 8.4 mm/min (87.7%/min deformation). Five (5) specimens were tested for each composition. A computer program called TestWorks 4 was used to collect data during testing and to generate a stress versus strain curve from which the average peak stress, break stress, elongation at break, and energy per volume at break were determined.

Expansion Ratio, Density, and Percent Void Volume

To determine expansion ratio, density, and percent void volume, the width (W_(i)) and thickness (T_(i)) of the specimen were initially measured prior to cold drawing. The length (L_(i)) before drawing was also determined by measuring the distance between two markings on a surface of the specimen. Thereafter, the specimen was cold drawn to initiate voiding. The width (W_(f)), thickness (T_(f)), and length (L_(f)) of the specimen was then measured to the nearest 0.01 mm utilizing Digimatic Caliper (Mitutoyo Corporation). The volume (V_(i)) before cold drawing was calculated by W_(i)×T_(i)×L_(i)=V_(i). The volume (V_(f)) after cold drawing was also calculated by W_(f)×T_(f)×L_(f)=V_(f). The expansion ratio (φ) was calculated by φ=V_(f)/V_(i); the density (P_(f)) of was calculated by: P_(f)=P_(i)/φ, where P_(i) is density of precursor material; and the percent void volume (% V_(v)) was calculated by: % V_(v)=(1−1/φ)×100.

Surface Roughness

Clean (air blown) surfaces of material were analyzed. The samples were analyzed using an FRT MicroProf® noncontact white light profilometer. The optical head used was the 100 μm z-range unit, calibrated before use. Z-sensitivity of this head was approximately 6 nanometers. 500 μm×500 μm and 1 mm×1 mm areas on each were analyzed. The 500-μm fields were sampled with 250 lines×250 points/line yielding sampling resolution=2-microns. The 1 mm scans were made using 400 lines×400 points/line for a sampling resolution of 2.5-microns. The resulting topographic maps were processed using FRT Mark III software to obtain the average surface roughness parameter, sPa.

Moisture Content

Moisture content may be determined using an Arizona Instruments Computrac Vapor Pro moisture analyzer (Model No. 3100) in substantial accordance with ASTM D 7191-05, which is incorporated herein in its entirety by reference thereto for all purposes. The test temperature (§X2.1.2) may be 130° C., the sample size (§X2.1.1) may be 2 to 4 grams, and the vial purge time (§X2.1.4) may be 30 seconds. Further, the ending criteria (§X2.1.3) may be defined as a “prediction” mode, which means that the test is ended when the built-in programmed criteria (which mathematically calculates the end point moisture content) is satisfied.

Example 1

A precursor material was formed from injection molded samples by extruding PLA 6201D (Natureworks®, melt flow rate of 10 g/10 minutes at 190° C.) into an injection molded doge bone bar. When attempted to be cold drawn at 50 mm/min draw rate (87.7%/min), the bar failed at just about 3% elongation.

Example 2

A precursor material was formed by injection molding of a dog bone shaped bar from a blend of 88.7 wt. % polylactic acid (PLA 6201D, Natureworks®), 9.9 wt. % of a toughening additive and 1.4% polyepoxide modifier. The toughening additive was VISTAMAXX™ 2120 (ExxonMobil), which is a polyolefin copolymer/elastomer with a melt flow rate of 29 g/10 min (190° C., 2160 g) and a density of 0.866 g/cm³. The polyepoxide modifier was poly(ethylene-co-methyl acrylate-co-glycidyl methacrylate) (LOTADER® AX8950, Arkema) having a melt flow rate of 70-100 g/10 min (190° C./2160 g), a glycidyl methacrylate content of 7 to 11 wt. %, methyl acrylate content of 13 to 17 wt. %, and ethylene content of 72 to 80 wt. %. The polymers were fed into a co-rotating, twin-screw extruder (ZSK-30, diameter of 30 mm, length of 1328 millimeters) for compounding that was manufactured by Werner and Pfleiderer Corporation of Ramsey, N.J. The extruder possessed 14 zones, numbered consecutively 1-14 from the feed hopper to the die. The first barrel zone #1 received the resins via gravimetric feeder at a total throughput of 15 pounds per hour. The die used to extrude the resin had 3 die openings (6 millimeters in diameter) that were separated by 4 millimeters. Upon formation, the extruded resin was cooled on a fan-cooled conveyor belt and formed into pellets by a Conair pelletizer. The extruder screw speed was 200 revolutions per minute (“rpm”).

The pellets were then flood fed into a Spritzgiessautomaten BOY 22D injection molded device. Temperature zones for the injection molding process ranged from 185° C. to 225° C., the injection holding pressure time was 10 sec to 14 sec, the cooling time of 25 sec to 50 sec, the cycle times ranged from 35 sec to 65 sec, and the mold temperature was set at about 21° C. or 10° C. The injection molded bar in a form of dog bone (ASTM D638) was drawn at a draw rate of 50 mm/min (87.7% deformation/min). The material deformed non-uniformly with localized stress whitened areas and demonstrated elongation at failure of only about 11% deformation.

Example 3

A precursor material was formed by injection molding of a dog bone shaped bar from a blend of 85.3 wt. % polylactic acid (PLA 6201 D, Natureworks®), 9.5 wt. % of VISTAMAXX™ 2120 (ExxonMobil), 1.4 wt. % polyepoxide modifier (LOTADER® AX8900, Arkema), and 3.8 wt. % internal interfacial modifier (PLURIOL® WI 285 Lubricant from BASF). The PLURIOL® WI285 was added via injector pump into barrel zone #2. Injection molded bars were formed from the blend as described in Example 2. The injection molded bars were initially extended to failure and demonstrated a deformation to break of more than 120%, which was beyond the limits of testing apparatus. During extension testing, the material initially stress whitened uniformly and homogeneously followed by localized necking around deformations of about 100% extension.

After testing the extensibility of the precursor material to failure, the precursor material bar was drawn to 50% elongation at a draw rate of 50 mm/min (87.7% deformation/min) as described in Example 1. The material uniformly stress whitened across the working length of the sample demonstrating the formation of a homogeneous and uniform voided structure. The volume increase due to micro-voiding was estimated to be about 57% and total volume expansion versus original volume of about 157%. The expansion ratio was 1.57 resulting in estimated percent void volume of 36% and estimated material density of about 0.76 g/cc based on a precursor material density of 1.19 g/cc and a PLA density of 1.25 g/cc. The voided material density was also measured independently by the liquid displacement method. This measurement provided a material density of 0.78 g/cc, which is close to the density estimated based on volume expansion ratio measurement. The longitudinal deformation in the voided material was E_(l)=60% (longitudinal strain of 0.60), the deformation in transverse direction was E_(t)=−1% (transverse strain in cross direction of −0.01), and the Poisson coefficient was 0.017, which also indicated a significant volume increase in the drawn material.

The small ASTM D638-10 Type V dog bone samples were also cut from the low density voided material to conduct tensile testing according to the standard ASTM D638-10 procedures and as described above. The low density material showed a tensile modulus of about 340 Mpa, peak stress of 38.4 Mpa, break stress of 38.4 Mpa, and elongation at break of 131%.

Example 4

A precursor material was formed by injection molding a ASTM D638-10 Type I dog bone shaped bar from a blend of 85.91 wt. % polylactic acid (PLA 6201D, Natureworks®), 9.55 wt. % of VISTAMAXX™ 2120 (ExxonMobil), 0.72 wt. % polyepoxide modifier (LOTADER® AX8900, Arkema), and 3.82 wt. % PLURIOL® WI 285 (BASF). The injection molded precursor material was drawn to about 76% strain as described in Example 3. The material demonstrated homogeneous and uniform stress-whitening and voiding. The expansion ratio was 1.95 resulting in estimated percent void volume of 49% and material density of about 0.61 g/cc based on precursor material density of 1.19 g/cc and PLA density of 1.25 g/cc. The Poisson coefficient was 0.06.

Example 5

A precursor material was formed by injection molding of a ASTM D638-10 Type I dog bone shaped bar from a blend of 84.5 wt. % polylactic acid (PLA 6201 D, Natureworks®), 9.4 wt. % of VISTAMAXX™ 2120 (ExxonMobil), 1.4 wt. % polyepoxide modifier (LOTADER® AX8900, Arkema), and 4.7 wt. % internal interfacial modifier HALLGREEN® IM-8830 from Hallstar. The HALLGREEN® IM-8830 was added via injector pump into barrel zone #2. Injection molded parts were formed from the blend. The injection molded precursor material was drawn to about 50% strain as described in Example 3, and demonstrated homogeneous and uniform stress-whitening and voiding. The expansion ratio was 1.26 resulting in estimated percent void volume of 21% and material density of about 0.94 g/cc based on precursor material density of 1.19 g/cc and PLA density of 1.25 g/cc. The Poisson coefficient was 0.01.

Example 6

A precursor material was formed by injection molding of a ASTM D638-10 Type I dog bone shaped bar from a blend of 85.3 wt. % polylactic acid (PLA 6201 D, Natureworks®), 9.5 wt. % of toughening additive ESCORENE™ UL EVA 7720 (ExxonMobil), 1.4 wt. % polyepoxide modifier (LOTADER® AX8900, Arkema), and 3.8% wt. % PLURIOL® WI 285 (BASF). The injection molded precursor material was drawn to about 50% strain as described in Example 3, and demonstrated homogeneous and uniform stress-whitening and voiding. The expansion ratio was 1.67 resulting in estimated percent void volume of 40% and material density of about 0.71 g/cc based on precursor material density of 1.19 g/cc and PLA density of 1.25 g/cc. The Poisson coefficient was 0.03. Notched impact testing was also conducted. The notched impact resistance was estimated to be about 6.31 joules/cm. During the test, the notch sample resisted notch propagation by bending, twisting, and plastically deforming. As a result of complex material response, the notch was stopped and material did not fail during the test. On average, five samples were tested for the impact resistance. Small ASTM D638-10 Type V dog bone samples were also cut from the low density voided material to conduct tensile testing according to the standard ASTM procedures. As a result of testing, the material showed a tensile modulus of about 522 Mpa, peak stress of 33.0 Mpa, break stress of 33.0 Mpa, and elongation at break of 103%.

Example 7

A precursor material was formed by injection molding of a ASTM D638-10 Type I dog bone shaped bar from a blend of 85.3 wt. % polylactic acid (PLA 6201D, Natureworks®), 9.5 wt. % of VISTAMAXX™ 2120 (ExxonMobil), 1.4 wt. % polyepoxide modifier (LOTADER® AX8900, Arkema), and 3.8 wt. % internal interfacial modifier (PLURIOL® WI 285 Lubricant from BASF). The injection molded precursor material was drawn to about 110% strain at a rate of 5 mm/minute. The expansion ratio was 2.01 resulting in estimated percent void volume of 50% and material density of about 0.59 g/cc based on precursor material density of 1.19 g/cc and PLA density of 1.25 g/cc. The Poisson coefficient was 0.04. SEM photomicrographs were also taken after the material was cold drawn and oxygen plasma etched. The results are shown in FIG. 2. As shown, the material demonstrated homogeneous and uniform stress-whitening and voiding. Oxygen plasma etched samples were also analyzed by a mercury intrusion method via an Autopore IV900 instrument to characterize its pore diameter, bulk density, and porosity. The samples had a median pore diameter of 0.0799 μm, an average pore diameter of 0.0398 μm, a bulk density of 0.6883 g/mL and a porosity of 44.8957%. In addition, the BET surface area was 21.61 m²/g, as determined via Tristar II 3020 V1.03 by Micromeritics Instrument Services.

Example 8

A precursor material was formed by injection molding of a ASTM D638-10 Type I dog bone shaped bar from a blend of 85.3 wt. % polylactic acid (PLA 6201 D, Natureworks®), 9.5 wt. % of VISTAMAXX™ 2120 (ExxonMobil), 1.4 wt. % polyepoxide modifier (LOTADER® AX8900, Arkema), and 3.8 wt. % internal interfacial modifier (PLURIOL® WI 285 Lubricant from BASF). The injection molded precursor material was drawn to about 50% strain at a rate of 5 mm/minute. The expansion ratio was 1.53 resulting in estimated percent void volume of 35% and material density of about 0.78 g/cc based on precursor material density of 1.19 g/cc and PLA density of 1.25 g/cc. The Poisson coefficient was 0.01. Notched impact testing was also conducted on the low density voided material. The notched impact resistance was estimated to be about 5.75 joules/cm. During the test, the notch sample resisted notch propagation by bending, twisting, and plastically deforming. As a result of this complex material response, the notch was stopped and material did not fail during the test. On average, five samples were tested for the impact resistance.

SEM photomicrographs were also taken after the material was cold drawn and impact testing was carried out. The results are shown in FIG. 3. As shown, the material demonstrated homogeneous and uniform stress-whitening and micro-voiding.

Example 9

A precursor material was formed from injection molded samples by extruding Crystar® 4434 polyethylene terephthalate (DuPont®) into an injection molded ASTM D638-10 Type I dog bone bar. When attempted to be cold drawn at 50 mm/min draw rate (87.7%/min), the bar failed at just about 3% elongation.

Example 10

A precursor material was formed by injection molding of a ASTM D638-10 Type I dog bone shaped bar from a blend of 85.3 wt. % polyethylene terephthalate (Crystar® 4434, DuPont®), 9.5 wt. % of VISTAMAXX™ 2120 (ExxonMobil), 1.4 wt. % polyepoxide modifier (LOTADER® AX8900, Arkema), and 3.8 wt. % internal interfacial modifier (PLURIOL® WI 285 Lubricant from BASF). The injection molded precursor material was drawn to about 50% strain at a rate of 5 mm/minute. The expansion ratio was 1.49 resulting in estimated percent void volume of 33% and material density of about 0.92 g/cc based on precursor estimated material density of 1.37 g/cc. The Poisson coefficient was 0.06.

Example 11

A precursor material was formed by injection molding of a ASTM D638-10 Type I dog bone shaped bar from a blend of 84.5 wt. % polylactic acid (PLA 6201D, Natureworks®), 9.4 wt. % of VISTAMAXX™ 2120 (ExxonMobil), 1.4 wt. % polyepoxide modifier (LOTADER® AX8900, Arkema), and 4.7 wt. % internal interfacial modifier HALLGREEN® IM-8830 from Hallstar. The HALLGREEN@IM-8830 was added via injector pump into barrel zone #2. Injection molded parts were formed from the blend. The injection molded precursor material was drawn to about 139% strain at 5 mm/min and demonstrated homogeneous and uniform stress-whitening and voiding. The expansion ratio was 2.33 resulting in estimated percent void volume of 57% and material density of about 0.51 g/cc based on precursor material density of 1.19 g/cc and PLA density of 1.25 g/cc. Surface topographic analysis showed the precursor material had an average roughness (sPA) of 0.134 μm. After cold drawing, the material had an average roughness of 0.907 μm. SEM photomicrographs were also taken after the material was cold drawn and impact testing was carried out. The results are shown in FIGS. 4-6. As shown, the material demonstrated homogeneous and uniform stress-whitening and micro-voiding.

Example 12

A precursor material was formed by injection molding of a ASTM D638-10 Type I dog bone shaped bar from a blend of 87.0 wt. % polylactic acid (PLA 6201 D, Natureworks®), 9.7 wt. % of VISTAMAXX™ 2120 (ExxonMobil), 1.4 wt. % polyepoxide modifier (LOTADER® AX8900, Arkema), and 1.9 wt. % internal interfacial modifier (PLURIOL® WI 285 Lubricant from BASF). The injection molded precursor material was drawn to about 50% strain at a rate of 5 mm/minute. The expansion ratio was 1.47 resulting in estimated percent void volume of 32% and material density of about 0.81 g/cc based on precursor material density of 1.19 g/cc and PLA density of 1.25 g/cc. The Poisson coefficient was 0.03.

Example 13

Samples were formed as described in Example 2, except the polyepoxide modifier was LOTADER® AX8900. The injection molded bar in a form of ASTM D638-10 Type I was drawn at a draw rate of 50 mm/min (87.7% deformation/min). The material deformed non-uniformly with localized stress whitened areas and demonstrated elongation at failure of only about 9% deformation.

While the invention has been described in detail with respect to the specific embodiments thereof, it will be appreciated that those skilled in the art, upon attaining an understanding of the foregoing, may readily conceive of alterations to, variations of, and equivalents to these embodiments. Accordingly, the scope of the present invention should be assessed as that of the appended claims and any equivalents thereto. 

1-34. (canceled)
 35. A thermoplastic composition comprising a rigid polyester having a glass transition temperature of about 0° C. or more, a polymeric toughening additive, and an interphase modifier, wherein the thermoplastic composition has a morphology in which a plurality of discrete primary domains and voids are dispersed within a continuous phase, the domains containing the polymeric toughening additive and the continuous phase containing the polyester, wherein the voids contain a combination of micro-voids having a dimension of about 1 micrometer or more and nano-voids having a dimension of less than about 1 micrometer, wherein the thermoplastic composition has a density of about 1.4 grams per cubic centimeter or less, and wherein the ratio of the glass transition temperature of the thermoplastic composition to the glass transition temperature of the polyester is from about 0.7 to about 1.3.
 36. The thermoplastic composition of claim 35, wherein the composition has a density of from about 0.5 grams per cubic centimeter to about 0.95 grams per cubic centimeter.
 37. The thermoplastic composition of claim 35, wherein the average percent volume of the composition that is occupied by the voids is from about 20% to about 80% per cubic centimeter.
 38. The thermoplastic composition of claim 35, wherein the aspect ratio of the micro-voids is from about 0.1 to about
 1. 39. The thermoplastic composition of claim 35, wherein the micro-voids have a dimension of about 1.5 micrometers or more.
 40. The thermoplastic composition of claim 35, wherein the nano-voids have a dimension of from about 25 nanometers to about 500 nanometers.
 41. The thermoplastic composition of claim 35, wherein the polyester includes polylactic acid, polyethylene terephthalate, or a combination thereof.
 42. The thermoplastic composition of claim 35, wherein the polyester has a glass transition temperature of from about 50° C. to about 75° C.
 43. The thermoplastic composition of claim 35, wherein the ratio of the solubility parameter for the polyester to the solubility parameter of the polymeric toughening additive is from about 0.5 to about 1.5, the ratio of the melt flow rate for the renewable polyester to the melt flow rate of the polymeric toughening additive is from about 0.2 to about 8, and the ratio of the Young's modulus elasticity of the polyester to the Young's modulus of elasticity of the polymeric toughening additive is from about 2 to about
 500. 44. The thermoplastic composition of claim 35, wherein the polymeric toughening additive includes a polyolefin.
 45. The thermoplastic composition of claim 44, wherein the polyolefin is a propylene homopolymer, propylene/la-olefin copolymer, ethylene/α-olefin copolymer, or a combination thereof.
 46. The thermoplastic composition of claim 35, wherein the polymeric toughening additive constitutes from about 1 wt. % to about 30 wt. % based on the weight of the polyester.
 47. The thermoplastic composition of claim 35, wherein the interphase modifier has a kinematic viscosity of from about 0.7 to about 200 centistokes, determined at a temperature of 40° C.
 48. The thermoplastic composition of claim 35, wherein the interphase modifier is hydrophobic.
 49. The thermoplastic composition of claim 35, wherein the interphase modifier is a silicone, silicone-polyether copolymer, aliphatic polyester, aromatic polyester, alkylene glycol, alkane diol, amine oxide, fatty acid ester, or a combination thereof.
 50. The thermoplastic composition of claim 35, wherein the interphase modifier constitutes from about 0.1 wt. % to about 20 wt. % based on the weight of the polyester.
 51. The thermoplastic composition of claim 35, wherein the composition comprises a polyepoxide modifier that includes an epoxy-functional (meth)acrylic monomeric component.
 52. The thermoplastic composition of claim 35, wherein the polyester constitutes about 70 wt. % or more of the thermoplastic composition.
 53. The thermoplastic composition of claim 35, wherein the composition exhibits a Poisson coefficient of about 0.1 or less.
 54. The thermoplastic composition of claim 35, wherein the composition exhibits an Izod notched impact strength of about 1 J/cm or more, measured at 23° C. according to ASTM D256-10 (Method A).
 55. The thermoplastic composition of claim 35, wherein the composition exhibits a tensile elongation at break of about 40% or more, measured at 23° C. according to ASTM D638-10.
 56. The thermoplastic composition of claim 35, wherein the composition has an average surface roughness of about 0.2 μm or more. 